Linear filament compression and torsion spring

ABSTRACT

A spring including a wire having an elasticity by which the wire is compressible by an external force to a first position at which first and second ends thereof of are separated by a first distance and when the force is removed or an electrical current applied, the wire is extensible in response to an internal spring force to a second position at which the wire is substantially straight. A spring assembly is disclosed including a plurality of inventive wires cross-coupled with a support structure consisting of a plurality of coaxial rings. In the assembly, the wires extend parallel to an axis through a center of the rings.

CLAIM OF PRIORITY

This application is a continuation of and claims the benefit of priorityunder 35 U.S.C. §120 to U.S. patent application Ser. No. 11/710,381,entitled “LINEAR FILAMENT COMPRESSION AND TORSION SPRING”, Filed on Feb.23, 2007, which is hereby incorporated by reference herein in itsentirety.

STATEMENT REGARDING GOVERNMENT FUNDING

This invention was developed in part as a result of funding provided bythe United States Government; specifically, contract numberN00024-03-C-6111, “Standard Missile 3 (SM-3) Through Completion” withNaval Sea Systems Command. As a result of this funding, the UnitedStates Government has certain rights in this invention.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to deployment mechanisms and systems. Morespecifically, the present invention relates to spring loaded deploymentmechanisms and systems used for space and other applications.

2. Description of the Related Art

Operation in space, underwater and other hostile environments requiresprecise and reliable operation of numerous mechanisms to secure, deploy,move, and release various components. Space vehicles, in particular,frequently contain mechanisms that must move by some combination ofsliding, rolling, or rotating and the successful operation thereof isusually mission-critical. For example, solar arrays are often stowed forlaunch, but once in space, are deployed to maximize exposure to the sun.Antennas are often deployed to maintain adequate signal strength.Remote-sensing optical payloads are often deployed to track a scene ofinterest or examine new targets as the space vehicle orbits. Internallenses and mirrors of optical sensors are often mounted on adjustablemechanisms to maintain or adjust focus or to reject undesirable signals.Space vehicles must maintain attitude either by spinning or by the useof flywheels or gyroscopes. All of these devices, and many others,depend upon the successful and long-term operation of moving mechanicalassemblies.

Many types of deployment mechanisms are known and used for variousapplications. For certain applications, spring-loaded deploymentmechanisms are ideally suited. Helical (coil) springs are typically usedfor spring-loaded spacecraft deployment. However, for some applications,there is a need to reduce the weight associated with the deploymentmechanism. In addition, the lateral stiffness of conventional helicalsprings is deficient for some applications.

Hence, a need remains in the art for a low-cost, lightweight spring forproviding a desired force in deployment at a given weight specificationwith enhanced lateral stability.

SUMMARY OF THE INVENTION

The need in the art is addressed by the novel spring of the presentinvention. Generally, the inventive spring includes at least one wirehaving an elasticity by which the wire is compressible by an externalforce to a first position at which first and second ends thereof of areseparated by a first distance and extensible in response to an internalspring force or stored energy to a second position at which the wire issubstantially straight, such that the first and second ends areseparated by a second distance, the second distance being substantiallygreater than the first distance.

In the illustrative embodiment, the spring is implemented with Nitinol™superelastic alloy. As an alternative, the wire can be a shape memoryalloy. In this case, the wire would be extensible in response to theapplication of current thereto.

In a more specific implementation, a spring assembly is disclosedincluding a plurality of such wires cross-coupled with a supportstructure consisting of a plurality of coaxial rings. In the assembly,the wires are parallel to an axis extending through a center of therings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a perspective view of a conventional helical spring assembly.

FIG. 2 is a perspective view of a spring assembly implemented inaccordance with an illustrative embodiment of the present teachings.

FIG. 3 is a perspective view of the spring of the illustrativeembodiment of the present invention in a fully extended configuration.

FIGS. 4 a-d are diagrams depicting various stages of compression andextension of the spring of FIG. 3 in a configuration without theintermediate support ring.

FIG. 5 is a magnified view of the inventive spring depicted in FIG. 4 d.

DESCRIPTION OF THE INVENTION

Illustrative embodiments and exemplary applications will now bedescribed with reference to the accompanying drawings to disclose theadvantageous teachings of the present invention.

While the present invention is described herein with reference toillustrative embodiments for particular applications, it should beunderstood that the invention is not limited thereto. Those havingordinary skill in the art and access to the teachings provided hereinwill recognize additional modifications, applications, and embodimentswithin the scope thereof and additional fields in which the presentinvention would be of significant utility.

FIG. 1 is a perspective view of a conventional helical spring assembly.As shown in FIG. 1, the conventional helical spring assembly 10′includes a helical spring 12′ which is typically implemented with asingle coil of wire which may or may not be wound around a tube 14′. Thetube is supported on a base 16′. The tubing may be required to providelateral stiffness for certain applications or the tubing may be part ofthe mechanism being deployed of which spacecraft deployment is oneexample.

FIG. 2 is a perspective view of a spring assembly implemented inaccordance with an illustrative embodiment of the present teachings. Asshown in FIG. 2, the assembly 10 includes a spring 20 of novel design.In accordance with the present teachings, the spring 20 includes pluralsubstantially straight wires e.g., 22, 24, 26 and 28. In accordance withthe present teachings, each wire has an elasticity or stored energy bywhich the wire is compressible by an external force to a first positionat which first and second ends thereof of are separated by a firstdistance and, when the force is removed or an electrical current isapplied in the case of shape memory alloy wire, the wire is extensiblein response to an internal spring force or released energy to a secondposition at which the wire is substantially straight, such that thefirst and second ends are separated by a second distance, the seconddistance being substantially greater than the first distance. In theillustrative embodiment, each wire is implemented with Nitinol,aluminum-copper, or other material that has the property ofsuperelasticity or shape memory, that is to say a reversible straincapacity of up to 10% or a stored energy due to an electrically orthermally reversible phase change in the material. Nitinol is availablefrom many manufacturers such as Nitinol Devices and Components ofFremont, Calif.

The wires e.g., 22, 24, 26 and 28 are cross-coupled with a supportstructure consisting in the illustrative embodiment of a plurality ofcoaxial rings 30, 32 and 34. In the assembly, the wires are parallel toan axis extending through a center of the rings. The first ring 30 isretained by flanges 40, 42, 44, 46, etc. in an upper tube 48. The wirese.g., 22, 24, 26 and 28 surround the periphery of the upper tube 48 anda lower tube 50 into which the upper tube reciprocates during thecompression and extension of the spring 20. That is, the diameters ofthe upper and lower tubes are dissimilar to allow for relativetranslation therebetween. A base 52 is provided at the bottom of thelower tube 50 into which the third ring 34 seats. The tubes 48 and 50are part of an assembly to be deployed and hence are not part of theinvention per se.

FIG. 3 is a perspective view of the spring of the illustrativeembodiment of the present invention in a fully extended configuration.The number of wires e.g., 22, 24, 26 and 28 in the spring 20 may bedetermined by one of ordinary skill in the art with respect to a givenspring force required and compression force to be used. In addition, thespring constant is determined by the number of wires, the diameter ofthe wires and the type of material used in construction. The length ofthe wires should be determined with respect to the desired length oftravel of the object to be deployed.

In the illustrative embodiment, the wires are made of Nitinol™,aluminum-copper, or other material that has the property ofsuperelasticity or shape memory as mentioned above with a diameter inthe range of 0.001-0.080 inches.

In addition, the number of support rings may vary based on therequirements of the application as well. As will be appreciated by thoseskilled in the art, the wires may be secured to the support rings by anysuitable means including crimping, brazing, bonding, etc. The supportrings 30, 32 and 34 may be fabricated of any suitable metal (e.g.,titanium, aluminum, etc.) or a composite material.

FIGS. 4 a-d are diagrams depicting various stages of compression andextension of the spring of FIG. 3. In FIG. 4 a, the spring 20 is fullyextended. In FIG. 4 b, the spring is initially compressed and the upperand lower rings 30 and 34 thereof are pressed toward each other. At thispoint, the wires are bent as shown. With additional compression, theupper and lower rings 30 and 34 move closer to each other and the wiresare further deformed as shown in FIG. 4 c. Finally, the spring is fullycompressed as shown in FIG. 4 d.

FIG. 5 is a magnified view of the inventive spring depicted in FIG. 4 d.Note that the wires or filaments 22 and 24 neatly stow with somerotation of one or more of the support rings 30 or 34. Use of anintermediate support ring 32 (not shown) allows the end rings 30 and 34to remain rotationally fixed and thus, in this configuration, theinvention may be used in any situation where a traditional helical orcoil spring might be used.

Thus, the present invention has been described herein with reference toa particular embodiment for a particular application. Those havingordinary skill in the art and access to the present teachings willrecognize additional modifications applications and embodiments withinthe scope thereof.

It is therefore intended by the appended claims to cover any and allsuch applications, modifications and embodiments within the scope of thepresent invention.

1. A spring comprising: a support structure that includes a plurality ofcoaxial rings, wherein said plurality of coaxial rings includes a firstend ring, a second end ring and an intermediate ring between said firstend ring and said second end ring; and a plurality of wires coupled viasaid support structure, each wire extending from the first ring to thesecond ring, each wire having an elasticity by which said wire iscompressible to a first position at which first and second ends thereofare separated by a first distance and extensible in response to aninternal spring force or stored energy to a second position at whichsaid wire is substantially straight, such that said first and secondends are separated by a second distance, said second distance beingsubstantially greater than said first distance, wherein said first endring is retained by flanges on a first tube that is positioned insidesaid plurality of wires.
 2. The spring of claim 1 wherein each said wireis a superelastic alloy.
 3. The spring of claim 1 wherein each said wireis a shape memory alloy.
 4. A method for providing a spring forcecomprising: providing a support structure that includes a plurality ofcoaxial rings, wherein said plurality of coaxial rings includes a firstend ring, a second end ring and an intermediate ring between said firstend ring and said second end ring; providing a plurality of wirescoupled via said support structure, each wire extending from the firstring to the second ring, said plurality of wires having an elasticity bywhich said wires are compressible by an external force to a firstposition at which first and second ends thereof are separated by a firstdistance and when said force is removed or an electrical currentapplied, extensible in response to an internal spring force or storedenergy to a second position at which said wires are substantiallystraight, such that said first and second ends are separated by a seconddistance, said second distance being substantially greater than saidfirst distance; and providing a first tube positioned inside saidplurality of wires, said first tube including flanges that retain saidfirst end ring.
 5. A compression spring assembly comprising: an uppertube; a lower tube that has a diameter different than said upper tubesuch that said upper and lower tubes move telescopically relative to oneanother; and a plurality of wires surrounding a periphery of said upperand lower tubes, each wire having an elasticity by which said wire iscompressible by an external force to a first position at which first andsecond ends thereof of are separated by a first distance and when saidforce is removed, said wire is extensible in response to an internalspring force to a second position at which said wire is substantiallystraight, such that said first and second ends are separated by a seconddistance, said second distance being substantially greater than saidfirst distance.
 6. The compression spring assembly of claim 5, whereinsaid wires are a superelastic alloy.
 7. The compression spring assemblyof claim 5, wherein said wires are a shape memory alloy.
 8. Thecompression spring assembly of claim 5, further comprising a supportstructure that couples said plurality of wires.
 9. The compressionspring assembly of claim 8, wherein said support structure includesfirst and second coaxial rings.
 10. A method for providing a springforce comprising: providing an upper tube and a lower tube that has adiameter different than said upper tube such that said upper and lowertubes move telescopically relative to one another; and providing aplurality of wires that surround a periphery of said upper and lowertubes, each of said wires having an elasticity by which said wires arecompressible by an external force to a first position at which first andsecond ends thereof are separated by a first distance and when saidforce is removed or an electrical current applied, extensible inresponse to an internal spring force or stored energy to a secondposition at which said wires are substantially straight, such that saidfirst and second ends are separated by a second distance, said seconddistance being substantially greater than said first distance.
 11. Themethod of claim 10 further comprising providing a support structure thatincludes a plurality of coaxial rings such that each of said coaxialrings couples said plurality of wires.
 12. The method of claim 10wherein providing a support structure that includes a plurality ofcoaxial rings includes providing a first end ring, a second end ring andan intermediate ring between said first end ring and said second endring.
 13. A compression spring assembly comprising: an upper tube; alower tube that has a diameter different than said upper tube such thatsaid upper and lower tubes move telescopically relative to one another;a plurality of wires surrounding a periphery of said upper and lowertubes, each wire having an elasticity by which said wire is compressibleby an external force to a first position at which first and second endsthereof of are separated by a first distance and when said force isremoved, said wire is extensible in response to an internal spring forceto a second position at which said wire is substantially straight, suchthat said first and second ends are separated by a second distance, saidsecond distance being substantially greater than said first distance;and a support structure that includes a plurality of coaxial rings suchthat each of said coaxial rings couples said plurality of wires, whereinsaid plurality of coaxial rings includes a first end ring, a second endring and an intermediate ring between said first end ring and saidsecond end ring.
 14. The compression spring assembly of claim 13,wherein said wires are a shape memory alloy.
 15. The compression springassembly of claim 13 wherein each wire is parallel to an axis extendingthrough a center of said coaxial rings.